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EN 3228:2010

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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Aerospace series - Nuts, hexagonal, plain, reduced height, normal across flats, in steel, cadmium plated - Classification: 900 MPa (at ambient temperature) / 235 °C

Superseded date

03-31-2022

Superseded by

EN 3228:2022

Published date

01-27-2010

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Foreword
1 Scope
2 Normative references
3 Required characteristics
4 Designation
5 Marking
6 Technical specification

This standard specifies the characteristics of plain, hexagonal nuts, reduced height, normal across flats, in steel, cadmium plated.Classification: 900 MPa / 235 °C.

Committee
ASD-STAN
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Superseded
SupersededBy

Standards Relationship
ONORM EN 3228 : 2010 Identical
NS EN 3228 : 2010 Identical
NEN EN 3228 : 2010 Identical
PN EN 3228 : 2010 Identical
NBN EN 3228 : 2010 Identical
BS EN 3228:2010 Identical
I.S. EN 3228:2010 Identical
UNE-EN 3228:2010 Identical
SN EN 3228 : 2010 Identical
DIN EN 3228:2010-05 Identical
NF EN 3228 : 2010 Identical

NFL 22-437 : C AIRCRAFT BOLTS AND NUTS - NUTS, HEXAGONAL, PLAIN, REDUCED HEIGHT NORMAL ACROSS FLATS, WITH LOCKING HOLES, ISO M OR ISO MJ THREADS, 4H5H OR 5H TOLERANCE CLASS ACCORDING TO DIAMETER
NFL 22-439 : B AIRCRAFT BOLTS AND NUTS - NUTS, HEXAGONAL, PLAIN, REDUCED HEIGHT, NORMAL ACROSS FLATS, WITH LOCKING HOLES, ISO M OR ISO MJ THREADS, 4H TOLERANCE CLASS
EN 2850:2017 Aerospace series - Carbon fibre thermosetting resin - Unidirectional laminates - Compression test parallel to fibre direction
BS EN 2850:2017 Aerospace series. Carbon fibre thermosetting resin - Unidirectional laminates. Compression test parallel to fibre direction
DIN EN 2644:1998-06 AEROSPACE SERIES - ROD ASSEMBLIES FOR FLIGHT CONTROLS - TECHNICAL SPECIFICATION
BS EN 2644:1998 Rod assemblies for flight controls. Technical specification
EN 2644:1998 Aerospace series - Rod assemblies for flight controls - Technical specification
NFL 22-461 : C AIRCRAFT BOLTS AND NUTS - NUTS, HEXAGONAL, PLAIN, REDUCED HEIGHT, NORMAL ACROSS FLATS, WITH LOCKING HOLES, ISO M OR ISO MJ THREADS, FINE PITCH THREADS, 4H5H TOLERANCE CLASS
I.S. EN 2850:2017 AEROSPACE SERIES - CARBON FIBRE THERMOSETTING RESIN - UNIDIRECTIONAL LAMINATES - COMPRESSION TEST PARALLEL TO FIBRE DIRECTION

EN 9100:2009 Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
ISO 8788:2000 Aerospace Nuts, metric Tolerances of form and position
ISO 5855-2:1999 Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts
PREN 3513 : 200P1 AEROSPACE SERIES - STEEL FE-PL711 - HARDENED AND TEMPERED - 900 <= R[M] <= 1100 MPA - BAR AND WIRE - D[E] <= 45 MM
EN 2438:2008 Aerospace series - Steel FE-PL2102 (35NiCr6) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm
ISO 9609:2016 Aerospace Nuts, hexagonal, plain, reduced height, normal across flats, with MJ threads, classifications: 450 MPa (at ambient temperature) /120 degrees C, 450 MPa (at ambient temperature) /235 degrees C, 600 MPa (at ambient temperature) /425 degrees C, 900 MPa (at ambient temperature) /235 degrees C, 900 MPa (at ambient temperature) /315 degrees C, 900 MPa (at ambient temperature) /650 degrees C, 1 100 MPa (at ambient temperature) /235 degrees C, 1 100 MPa (at ambient temperature) /730 degrees C and 1 250 MPa (at ambient temperature)/600 degrees C Dimensions
EN 2205:2009 Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm
EN 2133:2010 Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
TR 3823 : 2 AEROSPACE SERIES - MATERIALS FOR PLAIN, SLOTTED AND SELF-LOCKING BY PLASTIC RING HEXAGONAL NUTS
EN 2424:2008 Aerospace series - Marking of aerospace products
ISO 9139:1998 Aerospace — Nuts, plain or slotted (castellated) — Procurement specification
EN 2448:2008 Aerospace series - Steel FE-PL1503 (35CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bars - De ≤ 40 mm

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